CN201116540Y - Fan blade - Google Patents

Fan blade Download PDF

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Publication number
CN201116540Y
CN201116540Y CNU2007201881990U CN200720188199U CN201116540Y CN 201116540 Y CN201116540 Y CN 201116540Y CN U2007201881990 U CNU2007201881990 U CN U2007201881990U CN 200720188199 U CN200720188199 U CN 200720188199U CN 201116540 Y CN201116540 Y CN 201116540Y
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CN
China
Prior art keywords
blade
angle
degree
line
point
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
CNU2007201881990U
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Chinese (zh)
Inventor
张玲
任志杰
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Midea Group Co Ltd
Original Assignee
Midea Group
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Filing date
Publication date
Application filed by Midea Group filed Critical Midea Group
Priority to CNU2007201881990U priority Critical patent/CN201116540Y/en
Application granted granted Critical
Publication of CN201116540Y publication Critical patent/CN201116540Y/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Abstract

The utility model relates to a fan blade, including cylindrical impeller hub and the blade more than a slice, the line of each chord line mid point of above-mentioned blade of its characterized in that is curve L1, and the vertical line through blade central point O is L2, and L3 is the line of certain point on curve L1 and central point O, contained angle A between L2 and L31For the net bending angle of the blade, the connecting line passing through the root guide edge tangent point on the leeward side of the blade and the central point O is L4, and the included angle A between the tangent line L5 passing through a certain guide edge tangent point a on the leeward side of the blade and L42The angle is the leading edge bending angle, the radial included angle between the fan blade rotation plane and the hub is the blade installation angle Q, the ratio of the radius R of the hub to the maximum radius R of the blade is R/R of 0.2, 0.3, 0.4, 0.5, 0.6, 0.7, 0.8, 0.9 and 1.0, the net bending angle A of the blade is1Corresponding to 0 degree, 3 degree, 5 degree, 7 degree, 9 degree, 11 degree, 13 degree, 15 degree, 17 degree and guide edge bending angle A2The method comprises the following steps: 0 °, 3 °, 8 °, 11 °, 18 °, 25 °, 43 °, 65 °, 129 °, and the blade mounting angles Q are respectively 41 °, 35.5 °, 30.2 °, 23.5 °, 22.3 °, 20.2 °, 15.6 °, 12 °, 11 °. The utility model discloses owing to through preferred A1、A2And Q value, the purposes of improving air quantity and reducing noise can be achieved.

Description

A kind of fan fan blade
Technical field
The utility model is a kind of fan blade, particularly a kind of fan fan blade.
Background technique
At present, the part fan of selling on the market, there are problems such as the little and noise of air quantity is big in unreasonable because of fan blade design.
The model utility content
The purpose of this utility model aims to provide the fan fan blade that a kind of air quantity is big, noise is little, to overcome deficiency of the prior art.
A kind of fan fan blade by this purpose design, comprise centric leaf hub and a slice with upper blade, the line of wherein above-mentioned each mid-chord of blade is curve L1, and the vertical curve by blade central point 0 is L2, L3 is the line of last certain point of curve L1 with central point 0, the included angle A between L2 and the L 3 1Be the clean bending angle of blade, the line by blade lee face one lateral root portion guide margin point of contact and central point 0 is L4, by the tangent line L5 of a certain guide margin of blade lee face one side point of contact a and the included angle A of L4 2Be the guide margin bending angle, the radially angle of fan blade plane of rotation and leaf hub is blade angle Q, and leaf hub radius r is that r/R is 0.2,0.3,0.4,0.5 with the ratio of blade maximum radius R, 0.6,0.7,0.8,0.9, and 1.0 o'clock, the clean bending angle A of blade 1Should be 0 ° mutually, 3 °, 5 °, 7 °, 9 °, 11 °, 13 °, 15 °, 17 °, guide margin bending angle A 2Should be mutually: 0 °, 3 °, 8 °, 11 °, 18 °, 25 °, 43 °, 65 °, 129 °, blade angle Q should be 41 ° mutually, and 35.5 °, 30.2 °, 23.5 °, 22.3 °, 20.2 °, 15.6 °, 12 °, 11 °.
The utility model is because the clean bending angle A of blade 1, guide margin bending angle A 2The size of decision noise, blade angle Q works to the gas compression performance and promptly determines the size of air quantity, therefore, by preferred A 1, A 2, the Q value, not only can reach the purpose that improves air quantity but also reduce noise.
Description of drawings
Fig. 1 is a structural representation of the present utility model.
Fig. 2 is the side-looking structural representation of Fig. 1.
Embodiment
Below in conjunction with drawings and Examples the utility model is described in further detail.
Referring to Fig. 1, this fan blade comprises centric leaf hub 1 and three uniform blades 2, three blades 2 and leaf hub 1 are injected into one, the line of above-mentioned blade 2 each mid-chord is curve L1, vertical curve by blade central point 0 is L2, L 3 is the line of last certain point of curve L1 with central point 0, the included angle A between L2 and the L3 1Be the clean bending angle of blade, the line by blade lee face one lateral root portion guide margin point of contact and central point 0 is L4, by the tangent line L5 of a certain guide margin of blade lee face one side point of contact a and the included angle A of L4 2Be the guide margin bending angle, the radially angle of fan blade plane of rotation and leaf hub is blade angle Q, and leaf hub 1 radius r is that r/R is 0.2,0.3,0.4,0.5 with the ratio of blade 2 maximum radius R, 0.6,0.7,0.8,0.9, and 1.0 o'clock, the clean bending angle A of blade 1Should be 0 ° mutually, 3 °, 5 °, 7 °, 9 °, 11 °, 13 °, 15 °, 17 °, guide margin bending angle A 2Should be mutually: 0 °, 3 °, 8 °, 11 °, 18 °, 25 °, 43 °, 65 °, 129 °, blade angle Q should be 41 ° mutually, and 35.5 °, 30.2 °, 23.5 °, 22.3 °, 20.2 °, 15.6 °, 12 °, 11 °.Because the clean bending angle A of blade 1, guide margin bending angle A 2The size of decision noise, blade angle Q works to the gas compression performance and promptly determines air quantity, the size of wind speed, therefore, by preferred A 1, A 2, the Q value, can reach and both improve air quantity, wind speed reduces the purpose of noise again.

Claims (1)

1, a kind of fan fan blade, comprise centric leaf hub (1) and a slice with upper blade (2), it is characterized in that the line of each mid-chord of above-mentioned blade (2) is curve L1, the vertical curve by blade central point 0 is L2, L3 is the line of last certain point of curve L1 with central point 0, the included angle A between L2 and the L3 1Be the clean bending angle of blade, the line by blade lee face one lateral root portion guide margin point of contact and central point 0 is L4, by the tangent line L5 of a certain guide margin of blade lee face one side point of contact a and the included angle A of L4 2Be the guide margin bending angle, the radially angle of fan blade plane of rotation and leaf hub is blade angle Q, and leaf hub (1) radius r is that r/R is 0.2,0.3,0.4,0.5 with the ratio of blade maximum radius R, 0.6,0.7,0.8,0.9, and 1.0 o'clock, the clean bending angle A of blade 1Should be 0 ° mutually, 3 °, 5 °, 7 °, 9 °, 11 °, 13 °, 15 °, 17 °, guide margin bending angle A 2Should be mutually: 0 °, 3 °, 8 °, 11 °, 18 °, 25 °, 43 °, 65 °, 129 °, blade angle Q should be 41 ° mutually, and 35.5 °, 30.2 °, 23.5 °, 22.3 °, 20.2 °, 15.6 °, 12 °, 11 °.
CNU2007201881990U 2007-11-05 2007-11-05 Fan blade Expired - Lifetime CN201116540Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNU2007201881990U CN201116540Y (en) 2007-11-05 2007-11-05 Fan blade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNU2007201881990U CN201116540Y (en) 2007-11-05 2007-11-05 Fan blade

Publications (1)

Publication Number Publication Date
CN201116540Y true CN201116540Y (en) 2008-09-17

Family

ID=39991113

Family Applications (1)

Application Number Title Priority Date Filing Date
CNU2007201881990U Expired - Lifetime CN201116540Y (en) 2007-11-05 2007-11-05 Fan blade

Country Status (1)

Country Link
CN (1) CN201116540Y (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101936308A (en) * 2010-09-12 2011-01-05 美的集团有限公司 Fan blade
CN105257597A (en) * 2015-11-12 2016-01-20 珠海格力电器股份有限公司 Axial flow fan and axial flow fan blade thereof
US11365634B2 (en) 2018-11-16 2022-06-21 Rolls-Royce Plc Boundary layer ingestion fan system
US11364996B2 (en) 2018-11-16 2022-06-21 Rolls-Royce Plc Boundary layer ingestion fan system
US11365633B2 (en) 2018-11-16 2022-06-21 Rolls-Royce Plc Boundary layer ingestion fan system
US11370530B2 (en) 2018-11-16 2022-06-28 Rolls-Royce Plc Boundary layer ingestion fan system
US11414178B2 (en) 2018-11-16 2022-08-16 Rolls-Royce Plc Boundary layer ingestion fan system
US11486253B2 (en) 2018-11-16 2022-11-01 Rolls-Royce Plc Boundary layer ingestion fan system
US11486254B2 (en) 2018-11-16 2022-11-01 Rolls-Royce Plc Boundary layer ingestion fan system

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101936308A (en) * 2010-09-12 2011-01-05 美的集团有限公司 Fan blade
CN105257597A (en) * 2015-11-12 2016-01-20 珠海格力电器股份有限公司 Axial flow fan and axial flow fan blade thereof
CN105257597B (en) * 2015-11-12 2018-04-20 珠海格力电器股份有限公司 Axial flow fan and axial flow fan blade thereof
US11365634B2 (en) 2018-11-16 2022-06-21 Rolls-Royce Plc Boundary layer ingestion fan system
US11364996B2 (en) 2018-11-16 2022-06-21 Rolls-Royce Plc Boundary layer ingestion fan system
US11365633B2 (en) 2018-11-16 2022-06-21 Rolls-Royce Plc Boundary layer ingestion fan system
US11370530B2 (en) 2018-11-16 2022-06-28 Rolls-Royce Plc Boundary layer ingestion fan system
US11414178B2 (en) 2018-11-16 2022-08-16 Rolls-Royce Plc Boundary layer ingestion fan system
US11486253B2 (en) 2018-11-16 2022-11-01 Rolls-Royce Plc Boundary layer ingestion fan system
US11486254B2 (en) 2018-11-16 2022-11-01 Rolls-Royce Plc Boundary layer ingestion fan system

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
C56 Change in the name or address of the patentee

Owner name: MIDEA GROUP CO., LTD.

Free format text: FORMER NAME: MEIDI GROUP CO. LTD.

CP03 Change of name, title or address

Address after: 528311 Guangdong, Foshan, Beijiao, the United States, the United States and the United States on the avenue of the United States, the headquarters of the United States building B floor, District, 26-28

Patentee after: MIDEA GROUP Co.,Ltd.

Address before: 528311 Foshan, Shunde District, Beijiao Town, Penglai Road, the United States Industrial City

Patentee before: Midea Group

CX01 Expiry of patent term

Granted publication date: 20080917